JASC 5754
Service difficulty reports · 17,344
Reports filed under 5754 · Leading Edge Devices, newest first.
Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5754' ORDER BY difficulty_date DESC"
Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.
SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet' WHERE jasc_code = '5754' ORDER BY difficulty_date DESC
Run it at the DuckDB prompt, or in any tool that reads Parquet over HTTPS. More ways to query the release are on Use the data.
SDR DALA2023122110496Unknown · unknownLH SLAT TRACK #1 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028- 02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #1 LOWER PER ERA 60754314AD REV B, PRISDR DALA2023122110495Unknown · unknownRH SLAT TRACK #7 UPPER AND LOWER AT AFT ROLLER HAS CORROSION. "M " PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028-02A. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FURSDR DALA2023122110494Unknown · unknownLH SLAT TRACK # 10 LOWER SURFACE HAS CORROSION AT AFT ROLLER. EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H # 10 LOWER SLAT TRACK PER ERA 607543-14AD REV. B SDR DALA2023122110493Unknown · unknownLH SLAT TRACK#9 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #9 UPPER PER ERA 607543-14AD REV. B AND PRI RESDR DALA2023122110492Unknown · unknownRH SLAT TRACK #8 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION "M" PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028- 02B EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING SUPPOIRT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQSDR DALA2023122110491Unknown · unknownLH SLAT TRACK 9 LOWER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #9 LOWER PER ERA 607543-14AD REV. B AND PRI RESDR DALA2023122110490Unknown · unknownLH SLAT TRACK #8 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT REF AA 5742-01028-02A LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED L/H SLAT TRACK #8 UPPER PER ERA 607543-14AD REV. B AND PRSDR DALA2023122110489Unknown · unknownRH SLAT TRACK #6 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION. "M" PROVIDED TO ASSIST WITH LOCATION. EVIDENCE OF PREVIOUS IS PRESENT. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED . ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR FURTHER FLIGHTSDR DALA2023122110488Unknown · unknownLH SLAT TRACK #8 LOWER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED SLAT TRACK #8 LOWER PER ERA 667543-14AD REV B AND PRI REV. SDR DALA2023122110487Unknown · unknownLT SLAT TRACK #2 LOWER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS NOT PRESENT REF AA 5742-01028-02A . LIAISON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #2 LOWER PER ERA 607543-14AD REV. B AND PSDR DALA2023122110486Unknown · unknownRH SLAT TRACK #5 UPPER AT AFT ROLLER HAS CORROSION "M" PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028-02B. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIASON ENGINEERING SUPPORT WILL BE NEEDED REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED PRIOR TO FSDR DALA2023122110485Unknown · unknownLH SLAT TRACK #7 UPPER SURFACE HAS CORROSION AT AFT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #7 UPPER PER ERA 607543-14AD REV B AND PRI REV.SDR DALA2023122110484Unknown · unknownRH SLAT TRACK #4 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION. "M" PROVIDED TO ASSIST WITH LOCATION. REF AA WORK CARD NUMBER 5742-01028. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIASON ENGINEERING WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATIONSDR DALA2023122110483Unknown · unknownRH SLAT TRACK #2 LOWER AT AFT ROLLER HAS CORROSION. "M" PROVIDED TO ASSIST WITH LOCATION. REF AA WORK CARD #5742-01028B. EVIDENCE OF PREVIOUS REWORK (NOT PRESENT) LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQUIRED. RSDR DALA2023122110482Unknown · unknownLH SLAT TRACK #7 LOWER SURFACE HAS CORROSION AT ROLLER EVIDENCE OF PREVIOUS REWORK IS PRESENT. REF AA 5742-01028-02A LIASON ENGINEERING SUPPORT WILL BE REQUIRED PRIOR TO FURTHER FLIGHT. REPAIRED LH SLAT TRACK #7 LOWER PER ERA 607543-14AD REV. B AND PRI REV. 0 SDR DALA2023122110507Unknown · unknownRH SLAT TRACK #9 UPPER AT AFT ROLLER AND LOWER AFT ROLLER HAS CORROSION "M" PROVIDED TO ASSIST WITH LOCATION. REF 5742-01028- 02B. EVIDENCE OF PREVIOUS REWORK IS PRESENT. LIAISON ENGINEERING SUPPORT WILL BE REQUIRED. ADDITIONAL ENGINEERING DOCUMENTATION IS REQSDR SWAA2024011733620Angle · crackedCRACK ON INBOARD ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING 2023-761689<[01] REPLACED INBOARD ANGLE ON INBOARD AUXILIARY TRACK OF SLAT 8 AT RT WING IAW B737-700 SRM 51-40-02 MEASURE OF CRACK IS:L= 0.750' TOOL USED CALIPER P/N: 500-172-30 S/N:1523780SDR SWAA2024011733207Angle · crackedCRACK ON INBOARD ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 2 AT LT WING 2023-761672<[01] REPLACED INBOARD ANGLE LOCATED OUTBOARD AUXILIARY TRACK OF SLAT 2 AT LT WING IAW B737-700 SRM 51-40-02 MEASURE OF CRACK IS: L=0.750' TOOL USED CALIPER P/N: 500-172-30SDR SWAA2024010432389Slat · delaminated#8 SLAT T/E WEDGE LOWER SURFACE HAS A DELAM 4' FROM TOP 1' FROM O/B EDGE.<[01] REMOVED #8 SLAT IN REF TO AMM 27-81-21.;[02] OK TO INSTALL NEW #8 SLAT.;[03] INSTALLED NEW #8 SLAT PER M/M REF. 27-81-21.;[04] RII INSPECTION C/W FOR CA #3SDR AALA202312184853Skin · crackedAIRCRAFT IN BASE MAINTENANCE: CRACK IN RIGHT WING INBOARD LEADING EDGE SLAT NUMBER 8 SKIN AT WING STATION 250, INBOARD SLAT STATION 196. REPAIRED CRACK PER SRM 57-43-01-2R REPAIR 14.SDR UIEA2023121200986Unknown · unknownRH WING SLAT NO10 L/E CRACK(<P>RH WING SLAT NO 10 L/E CRACK IN THE SLAT #10, THE SKIN WHERE THE BREAK WAS LOCATED WAS REPAIRED. SRM 57-43-01-1A-1 AD1 REV 123 15AUG2023, SRM 57-43-01-2R-2 REV 123 15AUG2023. </P>)SDR UIEA2023121200987Unknown · unknownCRACK ON SLAT #9 AT OSS 641.74 AND 7.5" TO T/E, RH WING.(<P>CRACK ON SLAT #9 AT OSS 641.74 AND 7.5" TO T/E, RH WING. IN THE SLAT #9, THE SKIN WHERE THE BREAK WAS LOCATED WAS REPAIRED.</P>)SDR DALA2023121410269Access Panel · missingON WALKAROUND, FOUND LEFT WING SLAT MECHANISM LUBE ACCESS DOOR 521ADB MISSING. INSTALLED NEW ACCESS PANEL 521ADB PER B767 AMM 57-41 CDL.SDR DALA2023121310225Unknown · unknownSHIP 6817 AD - DISBOND OF 4.0IN LENGHT AND 2.5IN WIDTH WAS FOUND ON LH SLAT #4 LOWER SURFACE AT OSS 305.5, IN REFERENCE TO JOB 028-0001 CARD 5740-01145-05D. CORRECTIVE ACTION: SUMMARY OF NRC 00007:AD - DISBOND OF 4.0IN LENGHT AND 2.5IN WIDTH WAS FOUND ON LH SLSDR DALA2024061106030Slat · damagedSHIP 6715 REMOVE L/H WING SLAT #3 TO F.O.M. CORRECTIVE ACTION: REMOVED AND REPLACED L/H WING SLAT #3 I.A.W. B757 AMM 27-81-02 AND AMDS. (0102914)SDR SWAA2024012929283Skin · corroded#2 SLAT O/B UPPER AFT CORNER IS CORRODED.<[01] DISREGARD INSP ITEM DALE; MICHAEL STEPS 1;3;[02] STEP 2 PARTIAL ADJUSTMENT.;[03] COMPLETED STEP 4;[04] CERTIFIED;[05] CERTIFIED;[06] UPDATED RII;[07] CERTIFIED;[08] REMOVED AND REINSTALLED #2 SLAT PER AMM 27-81-21SDR DALA2023120810046Unknown · unknownSHIP 0670 DISBOND (2.000IN X 0.600IN) ON PRODUCTION DOUBLER AT OSS 305.5 LOWER SURFACE, LE SLAT 4 TRAILING EDGE WEDGE. LH WING. CORRECTIVE ACTION: SUMMARY OF NRC 00048: LOWER SURFACE ON SLAT 4 AT OSS 305.5 TRAILING EDGE WEDGE LH WING WAS REPAIRED PER B757-200 SDR SWAA2023121128353Skin · crackedCRACK ON RH INBD KRUEGER FLAP. REMOVED AND REPLACED #3 LE/FLAP (KRUEGER) PER AMM 27-81-11. REF. TTG8Q00Q3.SDR SWAA2023122126450Track · corrodedLEFT WING LEADING EDGE PANEL 521DB AFT SUPPORT HAS EVIDENCE OF CORROSION OUTBOARD OF INBOARD #4 SLAT AUXILIARY TRACK AT WS 279.<[01] UPDATED MEASUREMENT TABLE;[02] COMPLETED MEASUREMENT TABLE;[03] PARTIAL UPDATE FOR STEP 4;[04] COMPLETED STEP 3 PERFORMED WING SDR DALA2024012501163Slat · corrodedSHIP 5649 #8 SLAT HAS POSSIBLE CORROSION ON LEADING EDGE. DOT 45/003. CORRECTIVE ACTION: REMOVED AND INSTALLED NEW #8 SLAT ON AMDS T/C 2781-4380-01. ALL ADJUSTMENT AND OPS CHECK ACCOMPLISHED ON AMDS T/C. (0087902)SDR IPXA2023112998124Flap · warning message*EMERGENCY DECLARED* ON APPROACH LE FLAP DISAGREE LIGHT W/ EICAS CAUTION MESSAGE. WENT AROUND AND LANDED W/ FLAPS 20 USING ALTN FLAP EXTENSION CHECKLIST. PERFORMED FSEU BITE PER FIM 27-51-00/101 FIG 104. NO EXISTING FAULTS FOUND. PERFORMED FIM 27-81 FAULT TREESDR DALA2023112909796Unknown · unknownRE-WORKED SLAT TRACK #5 UPPER SURFACE AFT ROLLER. MAX. MATERIAL REMOVED 0.001", REMAINING THICKNESS TAPERS FROM .199" TO .200". UPPER SURFACE FWD ROLLER MAX. MATERIAL REMOVED 0.001", REMAINING THICKNESS 0.198", LOWER SURFACE FWD ROLLER. MAX. MATERIAL REMOVED 0SDR AALA202311282875Slat · warning messageAIRCRAFT WAS NOT GROUNDED: AN EMERGENCY WAS DECLARED COMMING INTO SFO DUE TO FLIGHT CONTROL SLATS LOCKED (JAMMED) FAULT MESSAGE DISPLAYED. THE AIRCRAFT LANDED SAFELY AT SFO. MAINTENANCE ACCOMPLISHED A SATISFACTORY OPERATIONAL CHECK OF THE FLAPS / SLAT SYSTEM WSDR SWAA2023112824352Skin · crackedCRACK LOWER SKIN SLAT 6 LEADING EDGE RT WING. PERFORMED PERMANENT REPAIR ON LOWER SKIN SLAT 6 LEADING EDGE RT WING IAW SRM 57-42-01-2R-8 AND SRM 51-40-02. PERFORMED PERMANENT REPAIR ON LOWER SKIN SLAT 6 LEADING EDGE RT WING IAW SRM 57-42-01-2R-8 AND SRM 51SDR AALA202311285857Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON RIGHT WING LEADING EDGE SLAT TRACK #10 LOWER FORWARD BOLT AT WS 11198 AND RIB 21. REPLACED BOLT PER AMM 27-84-66.SDR FDEA202311241892Wedge · delaminatedAD DISBOND INDICATION FOUND: #4 SLAT LOWER I/B SIDEE AT I/B STIFFENER, MARKED 5.5"L X 2.5"W COMPLETED PERMANENT REPAIR OF DISBOND FOUND ON #4 SLAT LOWER I/B SIDE AT I/B STIFFENER IAW FEDEX EA# F-5750-T0377026 TITLE WINGS - FLIGHT SURFACES.SDR DALA2023112809743Unknown · unknownSHIP 192 RHW NO.8 SLAT UPPER EDGE WORN AT LES 450. CORRECTIVE ACTION: REPAIRED RHW NO.8 SLAT UPPER EDGE WORN AT LES 450 AS PER B767- 300 SRM 57-43-02-2R-1 & SRM 51-70-10-2R-4 (0074884)SDR DALA2023112109606Unknown · unknownSHIP 3309 RHW #4 SLAT FOUND WITH DENT. CORRECTIVE ACTION: RHW #4 SLAT REPAIRED AS PER A330 SRM 57-40-00. (0073400)SDR IPXA2023113066828Flap · damaged*SUPPLEMENTAL SDR* L/H KRUGER FLAP SURROUND HAS DAMAGE STRUCTURE DAMAGE INSTALLED NEW UPPER SKIN RIBS & STRUCTURE REF SRM 51-40-21SDR IPXA2023112266828Unknown · unknown*SDR FILED OPEN* L/H KRUGER FLAP SURROUND HAS DAMAGE STRUCTURE DAMAGE REMOVED DAMAGED UPPER SKIN .RIBS & STRUCTURE FROM L/H KARMAN FAIRING REF SRM 53-15-63 & 51-40-21SDR IPXA2023112272262Unknown · unknown*SDR FILED OPEN* LEFT WING I/B SLAT I/B EDGE DAMAGESDR AALA2023112011402Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT SLAT TRACK 1 ON MID FORWARD BOLT ON RIGHT-HAND WING LOCATED AT WS 700 AND RIB 2. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202311205069Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT ON SLAT TRACK 2 UPPER FORWARD BOLT ON RIGHT-HAND WING LOCATED AT WS 1406 AND RIB 3. REPLACED BOLT PER TASK CARD 26C61057005.SDR AALA202311206058Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON BOLT ATTACHMENT SLAT TRACK 2 LOWER BOLT ON RIGHT-HAND WING LOCATED AT WS 1406 AND RIB 3. REPLACED BOLT PER TASK CARD 26C61057005.SDR IPXA2023113061044Flap · damagedDURING WALK AROUND FOUND EXTENSIVE DAMAGE TO LEFT WING KRUEGER FLAP. SEE TASK INFO FOR PHOTOS. ACCOMPLISHED AMM 27-88-11-0401 2C THRU END. ACCOMPLISHED AMM 27-87-11-0401 2D THRU END. ACCOMPLISHED AMM 27-87-14-0401 2E (4) THRU END. WITNESSED OPS CHECKS. RIG PINSDR GTIA2023112137633Slat · dentedDURING HMV FOUND DENT ON #3 SLAT. MDL 241MM MDW 22MM MDD 2.14MM OST 1.8MM RAF 329211301 CREATED. SDR REQUIRED.-VERIFIED NR #5001274242-0010 AND TC #1004125114-0010 (EA 5740-2375) REPAIR HAS BEEN ACCOMPLISHED IAW SPIRIT RAF-01 3292113-01. RE-INSPECTION NOT REQUSDR IPXA2023112061044Unknown · unknown*SDR FILED OPEN* DURING WALK AROUND FOUND EXTENSIVE DAMAGE TO LEFT WING KRUEGER FLAP. SEE TASK INFO FOR PHOTOSSDR DALA2023112109587Unknown · unknownSHIP 187 FOUND NO.11 SLAT EXTERNAL SKIN FROM OB TO IB 38 INCH CROSS TE TO LE 21 INCH BULGE. CORRECTIVE ACTION: NO. 11 SLAT EXTERNAL SKIN BULGE AREA REPAIRED AND FABRICATED THE REPLACEMENT NOSE RIB AS PER PRI: 613315-14 REV.0, COMPARED AND COMPLIED WITH ERA: 61SDR FDEA202311171861Slat · wornLH WING, SLAT NO. 5, INTERNAL UPPER SURFACE, NEAR INBOARD TRACK AREA WITH WEAR IN PREVIOUS REPAIR. LH WING, SLAT NO. 5, INTERNAL SURFACE, NEAR INBOARD TRACK AREA WAS REPAIRED IAW B767 SRM 57-43-02-2R FIG 201 SHEET 1-2 AND SRM 51-70-10-2R, FIG 202 PAGE 150,SDR AALA202311206562Bolt · corrodedAIRCRAFT IN BASE MAINTENANCE: CORROSION ON SLAT TRACK 9 SLAT 4 LOWER BOLT ON LEFT-HAND WING. REPLACED BOLT PER AMM 27-84-66-400-002-A.
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